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THE STATIC AERODYNAMIC CHARACTERISTICS OF A VARIABLE SWEEP WING RESEARCH MODEL.

John M. Durkin, David G. Lee

Abstract

A wind tunnel study was conducted to determine the effect of Mach number, angle of attack, and wing sweep angle on the longitudinal aerodynamic characteristics of a variable sweep wing research model. The study was conducted at Mach numbers between 0.60 and 1.15 and at angles of attack from -2 to 16 degrees. The report presents the data for the static phase of the investigation. (Author)

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Available abstract

Key concepts: Angle of attack, Mach number, Aerodynamics, Wing, Wind tunnel, Aerospace engineering, Variable (mathematics), Longitudinal static stability